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The contribution of this paper is the development of the levitation force as a function of the specimen velocity.
Results are presented in the form of S N curves, showing the variation of the fatigue strength as a function of the specimen orientation.
In this paper a general polynomial formula for the stress intensity factory under 20 kHz loading conditions is obtained using a finite element modeling approach as a function of the specimen's material properties and position and size of the internal crack.
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The arrest function of this specimen is produced by the compressive waves set off from the two inclined bottoms, and the horizontal components of these compressive waves have the confining action on the propagating cracks.
The modal testing has been performed by measuring frequency response functions of the specimens using an impact hammer and an accelerometer.
For the dynamic testing, an instrumented impact hammer and an accelerometer have been used to obtain the frequency response functions of the specimens at different temperatures.
Open image in new window Fig. 4 Probability functions of the specimens: a (P_{ii}(r)) for L3 sample, b (P_{ii}(r)) for L6 sample, c (P_{ii}(r)) for L9 sample, d (L_{i}(r)) for L3 sample, e (L_i(r)) for L6 sample, f (L_i(r)) for L9 sample (Note D is the edge length of the sample, and r is the distance between two points).
As the response of the actuator is a function of specimen, the actuator model involves boundary conditions of the experimental setup.
Open image in new window Fig. 8 Precision assessment of the adopted 3D DIC system for the derived strain measurements for specimen B103: a standard deviation of the horizontal strain (s_{epsilon _{x}}) as a function of the location on the specimen; b standard deviation of the vertical strain (s_{epsilon _{y}}) as a function of the location on the specimen.
Open image in new window Fig. 5 Precision assessment of the adopted Krypton K600 CMM for the derived strain measurements: a standard deviation of the horizontal strain (s_{epsilon _{x}}) as a function of the location on the specimen; b standard deviation of the vertical strain (s_{epsilon _{y}}) as a function of the location on the specimen.
Elaborate data acquisition schemes with autotuning functions minimize exposure of the specimen to the electron beam and sophisticated image analysis routines retrieve a maximum of information from noisy data sets.
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